What was found
ON LT WING LOWER SKIN PANEL AFT FROM PYLON NR 1 ARE ELONGATED HOLES ON HYDRAULIC FITTINGS. REPAIR WAS PERFORMED IAW RAS/BAE/1003815/2006 ISSUE: A, APPROVED BY EA 6-5720-103392.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON LT WING LOWER SKIN PANEL AFT FROM PYLON NR 1 ARE ELONGATED HOLES ON HYDRAULIC FITTINGS. REPAIR WAS PERFORMED IAW RAS/BAE/1003815/2006 ISSUE: A, APPROVED BY EA 6-5720-103392.